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    Institute of the Aeronautical Sciences Annual Meeting

    Summaries of Papers Presented to the 23rd Annual General Meeting Held in New York on January 24–27, 1955
    Emerald Group Publishing | 1955

    Hypersonic characteristics of an advanced aerospace plane

    MCCANDLESS, R. / CRUZ, C. | AIAA | 1985

    The lightning threat to aerospace vehicles

    RUSTAN, JR., P. | AIAA | 1985

    On convergence of computation of chemically reacting flows

    PARK, C. | AIAA | 1985

    Current status of numerical solutions of the Navier-Stokes equations

    MACCORMACK, R. | AIAA | 1985

    A new class of high accuracy TVD schemes for hyperbolic conservationlaws

    CHAKRAVARTHY, S. / OSHER, S. | AIAA | 1985

    Recent improvements in efficiency, accuracy, and convergence for implicit approximate factorization algorithms

    PULLIAM, T. / STEGER, J. | AIAA | 1985

    On the Drag Reduction of the Shark Skin

    BECHERT, D. / REIF, W | AIAA | 1985

    Application of a new class of high accuracy TVD schemes to the Navier-Stokes equations

    CHAKRAVARTHY, S. / SZEMA, K.-Y. / GOLDBERG, U. et al. | AIAA | 1985

    Circulation control airfoils - Past, present, future

    WOOD, N. / NIELSEN, J. | AIAA | 1985

    A multistage time-stepping scheme for the Navier-Stokes equations

    SWANSON, R. / TURKEL, E. | AIAA | 1985

    Artificial dissipation models for the Euler equations

    PULLIAM, T. | AIAA | 1985

    Laminar boundary layer stability experiments on a cone at Mach 8. III - Sharp cone at angle of attack

    STETSON, K. / THOMPSON, E. / DONALDSON, J. et al. | AIAA | 1985

    Afterbody drag reduction by vortex generators

    CALARESE, W. / CRISLER, W. / GUSTAFSON, G. | AIAA | 1985

    SUBSONIC PANEL METHODS - A COMPARISON OF SEVERAL PRODUCTION CODES

    MARGASON, RICHARD / KJELGAARD, SCOTT / SELLERS, III, WILLIAM et al. | AIAA | 1985

    Calculation of steady flow about propellers by means of a surface panel method

    HESS, J. / VALAREZO, W. | AIAA | 1985

    A simplified guidance algorithm for lifting aeroassist orbital transfer vehicles

    CERIMELE, C. / GAMBLE, J. | AIAA | 1985

    Numerical solution of unsteady viscous flow past rotor sections

    SANKAR, N. / TANG, W. | AIAA | 1985

    STS-8 atomic oxygen effects experiment

    VISENTINE, J. / LEGER, L. / KUMINECZ, J. et al. | AIAA | 1985

    Navier-Stokes computations for exotic airfoils

    BARTH, T. / PULLIAM, T. / BUNING, P. | AIAA | 1985

    Experimental studies of the effects of asymmetric transition on the aerothermal characteristics of hypersonic blunted slender cones

    HOLDEN, M. | AIAA | 1985

    Grid adaptation for the 2-D Euler equations

    DANNENHOFFER, III, J. / BARON, J. | AIAA | 1985

    A finite volume method for the calculation of compressible chemically reacting flows

    BUSSING, T. / MURMAN, E. | AIAA | 1985

    Direct simulation of a turbulent inner flow by finite-difference method

    KAWAMURA, T. / KUWAHARA, K. | AIAA | 1985

    Supercritical airfoil drag reduction by passive shock wave/boundary layer control in the Mach number range .75 to .90

    NAGAMATSU, H. / FICARRA, R. | AIAA | 1985

    The influence of camber variation on the aerodynamics of civil transport aircraft

    SZODRUCH, J. | AIAA | 1985

    The joined wing - An overview

    WOLKOVITCH, J. | AIAA | 1985

    An implicit, conservative, zonal-boundary scheme for Euler equation calculations

    RAI, M. | AIAA | 1985

    Euler computations of AGARD Working Group 07 airfoil test cases

    PULLIAM, T. / BARTON, J. | AIAA | 1985

    A relaxation approach to patched-grid calculations with the Euler equations

    RAI, M. | AIAA | 1985

    Solution method for a hovering helicopter rotor using the Euler equations

    ROBERTS, T. / MURMAN, E. | AIAA | 1985

    A study of compressible turbulent free shear layers using laser Doppler velocimetry

    PETRIE, H. / SAMIMY, M. / ADDY, A. | AIAA | 1985

    Interrelated effects of pitch rate and pivot point on airfoil dynamic stall

    HELIN, H. / WALKER, J. | AIAA | 1985

    An experimental investigation of an airfoil undergoing large amplitude pitching motions

    WALKER, J. / HELIN, H. / STRICKLAND, J. | AIAA | 1985

    Numerical experiments on subcritical transition mechanisms

    ZANG, T. / HUSSAINI, M. | AIAA | 1985

    A consideration of atomic oxygen interactions with space station

    LEGER, L. / VISENTINE, J. / SCHLIESING, J. | AIAA | 1985

    AN IMPLICIT PARABOLIZED NAVIER-STOKES SCHEME FOR HIGH ALTITUDE REENTRY FLOW

    BHUTTA, B.A. / LEWIS, C.H. | AIAA | 1985

    A comparison of Euler and Navier-Stokes solutions for supersonic flow over a conical delta wing

    NEWSOME, R. | AIAA | 1985

    Simulation of impinging turbulent jets

    CHILDS, R. / NIXON, D. | AIAA | 1985

    Numerical optimization design of advanced transonic wing configurations

    COSENTINO, G. / HOLST, T. | AIAA | 1985

    Icing flight research - Aerodynamic effects of ice and ice shape documentation with stereo photography

    MIKKELSEN, K. / MCKNIGHT, R. / RANAUDO, R. et al. | AIAA | 1985

    Ion beam sputter-deposited thin film coatings for protection of spacecraft polymers in low earth orbit

    BANKS, B. / MIRTICH, M. / RUTLEDGE, S. et al. | AIAA | 1985

    Numerical solution of the full-potential equation for rotors and oblique wings using a new wake model

    CHANG, I.-C. / TUNG, C. | AIAA | 1985

    Experiments on the stability of crossflow vortices in swept-wing flows

    SARIC, W. / YEATES, L. | AIAA | 1985

    The Goertler instability on an airfoil

    MANGALAM, S. / DAGENHART, J.R. / MEYERS, J. et al. | AIAA | 1985

    Noise from shock tube facilities

    SCHMIDT, E. / DUFFY, S. | AIAA | 1985

    Application of axisymmetric analogue for calculating heating in three-dimensional flows

    HAMILTON, H. / WEILMUENSTER, K. / DEJARNETTE, F. | AIAA | 1985

    A THREE-DIMENSIONAL INCOMPRESSIBLE PLOW SIMULATION METHOD AND ITS APPLICATION TO THE SPACE SHUTTLE MAIN ENGINE - Part I - Laminar Flow

    CHANG, JAMES / KWAK, DOCHAN / DAO, SAMUEL et al. | AIAA | 1985

    Unsteady aerodynamics of an airfoil encountering a passing vortex

    WU, J. / SANKAR, N. / HSU, T. | AIAA | 1985

    3D-Euler calculations using characteristic flux extrapolation

    EBERLE, A. | AIAA | 1985

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